rocket oxidizer
基本解釋
- 火箭氧化劑
英漢例句
- The ablative property requirements and the studies on the insulation layer of solid rocket engine in oxidizer rich environment were presented.
介紹了富氧環(huán)境下固體火箭發(fā)動(dòng)機(jī)對(duì)絕熱層性能的要求,以及在該特殊條件下對(duì)絕熱層所開展的研究工作。 - Results of subscale engine test show that the insulation (PFDH-2) can be used for heat protection of oxidizer rich solid rocket engine chamber.
試車結(jié)果表明,PFDH-2絕熱層可以對(duì)富氧環(huán)境下工作的發(fā)動(dòng)機(jī)燃燒室實(shí)施有效熱防護(hù)。 - An engine that obtains the oxygen needed from the atmosphere, used especially to propel aircraft and distinguished from rocket engines having self-contained fuel-oxidizer systems.
無內(nèi)含供氧系統(tǒng)的發(fā)動(dòng)機(jī):一種從空氣中獲得所需氧氣的發(fā)動(dòng)機(jī),尤用于推進(jìn)飛機(jī)飛行,并以擁有自帶燃料氧化系統(tǒng)區(qū)別于火箭發(fā)動(dòng)機(jī)。
odict.net